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Dynamic-measurement system modeling of spinning spacecraft attitude and their applications
KTH, School of Computer Science and Communication (CSC), Theoretical Computer Science, TCS. Nanjing University of Science and Technology, China .
KTH, School of Computer Science and Communication (CSC), Theoretical Computer Science, TCS.ORCID iD: 0000-0002-9706-5008
2007 (English)In: Chinese Space Science and Technology, ISSN 1000-758X, Vol. 27, no 4, 1-6+20 p.Article in journal (Refereed) Published
Abstract [en]

The modeling analysis technique is one of the most important approaches in space-flight mission. Based on the dynamical analysis, the copling models of the attitudes with angle velocities were successfully decoupled into two series independently differential equations. And, these two series models were integrated into an extended dynamic-measurement system with joint relationship equations. This new integrated model could be widely used in attitude determination, attitude control and attitude monitoring of the spinning spacecraft. Based on this integrated model, a series of practical algorithms were described to estimate attitude as well as spinning angles velocities with high precision.

Place, publisher, year, edition, pages
2007. Vol. 27, no 4, 1-6+20 p.
Keyword [en]
Attitude control, Joint relationship equation, Mathematical model, Spinning, Vehicle
National Category
Other Engineering and Technologies
URN: urn:nbn:se:kth:diva-155610ScopusID: 2-s2.0-35349020540OAI: diva2:762036

QC 20141110

Available from: 2014-11-10 Created: 2014-11-07 Last updated: 2014-11-10Bibliographically approved

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